Diamond DA40-TDI G1000

Compiled by Peter Schmidleitner © Peter Schmidleitner Engine Indication System Default page Display when pushing the SYSTEM button Display when pushing the FUEL button Compiled by Peter Schmidleitner © Peter Schmidleitner Default page Display when pushing the SYSTEM button Display when pushing the FUEL button Engine Indication System Upper part always the same LOAD is not measured, but calculated from common rail fuel pressure, ECU commanded injection time, manifold pressure and Prop RPM Compiled by Peter Schmidleitner © Peter Schmidleitner Engine Indication System Default SYSTEM FUEL Fuel Flow is not measured, but calculated from fuel pressure and ECU commanded injection time 18/03/14 15 Compiled by Peter Schmidleitner © Peter Schmidleitner NAV and COM Tuning LH identical RH Compiled by Peter Schmidleitner © Peter Schmidleitner NAV COM NAV and COM Tuning Compiled by Peter Schmidleitner © Peter Schmidleitner MHz tuning Active: inside Standby: outside Active: green Standby cursor: boxed COM volume/squelch COM KHz tuning COM flip-flop Cursor toggle Active („green“) is selected on AUDIO panel Garmin 1000 Compiled by Peter Schmidleitner © Peter Schmidleitner NAV Active: inside Standby: outside Active: green Standby cursor: boxed NAV volume ident filter MHz tuning KHz tuning NAV flip-flop Cursor toggle Active („green“) is on HSI, selected by CDI key Garmin 1000 18/03/14 16 Compiled by Peter Schmidleitner © Peter Schmidleitner Audio panel COM Split Switch Intercom Isolation „MIC“ selector; automatically selects corresponding Audio to headphone GMA 1347 Compiled by Peter Schmidleitner © Peter Schmidleitner Audio panel Marker Audio selectors Audio selectors Compiled by Peter Schmidleitner © Peter Schmidleitner Audio panel Clearance recorder playback Intercom volume and squelch control • Last 2,5 minutes of communication „MAN Squelch“ key Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Hydraulic System 18/03/14 17 Compiled by Peter Schmidleitner © Peter Schmidleitner Hydraulic brakes Pilot applies brake Compiled by Peter Schmidleitner © Peter Schmidleitner Hydraulic brakes Copilot applies brake Compiled by Peter Schmidleitner © Peter Schmidleitner Hydraulic brakes One-way valve is closed Parking brake „Pumping“ Pressure builds up Compiled by Peter Schmidleitner © Peter Schmidleitner Parking brake 18/03/14 18 Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Power Plant Compiled by Peter Schmidleitner © Peter Schmidleitner n Thielert Aircraft Engine TAE125-02-99 n Previously: TAE125-01 n Four cylinders, liquid-cooled n 1991 ccm (TAE125-01: 1689 ccm) n Common-rail direct injection n Reduction gear 1:1,69 n Dual digital engine control n Turbocharger n Max. power: 99kW (135 HP) at 2300 RPM n Max cont. power: 99kW (135 hp) at 2300 RPM Diamond DA40 TDI Engine Compiled by Peter Schmidleitner © Peter Schmidleitner n Thielert Aircraft Engine TAE125-02-99 n Previously: TAE125-01 n Four cylinders, liquid-cooled n 1991 ccm (TAE125-01: 1689 ccm) n Common-rail direct injection n Reduction gear 1:1,69 n Dual digital engine control n Turbocharger n Max. power: 99kW (135 HP) at 2300 RPM n Max cont. power: 99kW (135 hp) at 2300 RPM Diamond DA40 TDI Engine Compiled by Peter Schmidleitner © Peter Schmidleitner Digital Engine Control n ECU n Engine Control Unit this is a n FADEC n Full Authority Digital Engine Control 18/03/14 19 Compiled by Peter Schmidleitner © Peter Schmidleitner ECU – Engine Control Unit Compiled by Peter Schmidleitner © Peter Schmidleitner E.O.T. – Engine Order Telgraph („Chadburn“) Compiled by Peter Schmidleitner © Peter Schmidleitner • Power lever selects power (LOAD in %) • RPM automatically determined by selected power Diamond DA40 TDI Engine Compiled by Peter Schmidleitner © Peter Schmidleitner Diamond DA40 TDI Engine Engine air filter Alternate air valve Heat Exchanger for Cabin Heat System 18/03/14 20 Compiled by Peter Schmidleitner © Peter Schmidleitner Intercooler Diamond DA40 TDI Engine Compiled by Peter Schmidleitner © Peter Schmidleitner Diamond DA40 TDI Engine Coolant Heat Exchanger Reduction Gear Coolant Reservoir Generator Compiled by Peter Schmidleitner © Peter Schmidleitner Power plant – Gear oil Compiled by Peter Schmidleitner © Peter Schmidleitner Power plant – Gear oil 18/03/14 21 Compiled by Peter Schmidleitner © Peter Schmidleitner Power plant – Gear oil Is this the little bubble ? Compiled by Peter Schmidleitner © Peter Schmidleitner Power plant limitations n Italic figures are for the „old“ 125-01 engine n Max RPM: 2300 n Oil pressure: 1.0 – 6.5 bar n Oil quantity (per engine): 4.5 – 6.0 liters n Max. oil consumption: 0.1 liters/hr n Oil temperature: -30 (-32) °C – 140 °C n Gearbox temperature: max. 120 °C n Coolant temperature: -30 (-32) °C – 105 °C n Max. restart altitude: 8000 ft (6500 ft), 73–120 KIAS Compiled by Peter Schmidleitner © Peter Schmidleitner n Fuel: JET A-1 or JET A (ASTM D 1655) JET No. 3 (GB6537-94) Diesel (EN 590) n Oil: SHELL Helix Ultra 5W30 synth. API SL/CF SHELL Helix Ultra 5W40 synth. API SL/CF AERO SHELL Diesel 10W-40 n Gearbox oil: SHELL EP 75W90 API GL-4 n Coolant: DAI-G30-MIX special water (TAE-125-OM-02-01) + cooler protection 1:1 (BASF Glysantin Alu Protect Plus/G30) (freezing point –36 °C) ! Power plant fluid specifications Compiled by Peter Schmidleitner © Peter Schmidleitner „Diesel“ limitations n Temperature limits n Below -5° C no engine start n Below +5° C no take-off n Be sure that no diesel fuel is in the tanks – otherwise temp limitations for diesel ops must be observed 18/03/14 22 Compiled by Peter Schmidleitner © Peter Schmidleitner n When is no more diesel in the tanks? n each tank to be refilled at least twice with more than n 10,6 USG (40 ltrs) (normal tanks) n 17,2 USG (65 ltrs) (long range tanks) of Jet fuel otherwise n tank must be drained „Diesel“ limitations Compiled by Peter Schmidleitner © Peter Schmidleitner JET fuel Fuel temperature -30 -5 +5 +70 +75 Diesel, Diesel/JET blend or unknown Engine start Take-off Analogue indication FUEL page „Diesel“ limitations Default page Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Cooling System Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Cooling System 18/03/14 23 Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Cooling System Coolant Temp. < 80° Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Cooling System Coolant Temp. > 80° Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Cooling System Cabin Heat Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Cabin Heat 18/03/14 24 Compiled by Peter Schmidleitner © Peter Schmidleitner Cockpit DA 40 TDI Ventilation Cabin Cabin Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Ventilation Left wing Rear cabin ventilation air inlet Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Turbocharger System Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Turbo Charger Exhaust gas drives turbine Bypass for excess exhaust gas 18/03/14 25 Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Turbo Charger Turbine drives compressor Compressor compresses intake air Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Fuel System Compiled by Peter Schmidleitner © Peter Schmidleitner n 2 x 14 USG usable n = 28 USG n = 85 kg n At 70% power: ~ 5 USG/hr DA 40 TDI Fuel System Compiled by Peter Schmidleitner © Peter Schmidleitner n Long Range Tanks: 2 x 19,5 USG usable n = 39 USG n = 120 kg n Max indicated fuel per tank: 15 USG n Max. unbalance: 9 USG DA 40 TDI Fuel System 18/03/14 26 Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Fuel System Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Fuel System Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Fuel System 18-21 USG/hr ~60 USG/hr Fuel cooler Compiled by Peter Schmidleitner © Peter Schmidleitner Fuel cooler Right wing Air inlet Air outlet 18/03/14 27 Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Fuel System U/S Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 TDI Fuel System 18-21 USG/hr U/S Fuel cooler Compiled by Peter Schmidleitner © Peter Schmidleitner DA 40 Fuel system „Alternate means for fuel quantity indication“ Position: at the bore in the stall strip Compiled by Peter Schmidleitner © Peter Schmidleitner Fuel vents 18/03/14 28 Compiled by Peter Schmidleitner © Peter Schmidleitner Fuel tank drain FWD Compiled by Peter Schmidleitner © Peter Schmidleitner Fuel gascolator drain Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Electrical System Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System 18/03/14 29 Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System Power sources Generator 12-14V 90A Main Battery 12V 45Ah ECU Backup Battery 12V 12Ah Excitation Battery 12V 1,3 Ah Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System Power distribution Hot Battery Bus Battery Bus Main Bus Essential Bus ECU Bus Avionic Bus Compiled by Peter Schmidleitner © Peter Schmidleitner Electric Master, Essential Bus Compiled by Peter Schmidleitner © Peter Schmidleitner Engine Master 18/03/14 30 Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System OFF ON OFF Before Engine Start Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF Preparing Engine Start ON Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF ON Engine Start START Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System ON OFF ON ON After Engine Start 18/03/14 31 Compiled by Peter Schmidleitner © Peter Schmidleitner External Power Receptable Compiled by Peter Schmidleitner © Peter Schmidleitner External Power Receptable Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System OFF OFF GND PWR, El. Master OFF OFF Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System OFF OFF GND PWR, El. Master ON ON 18/03/14 32 Compiled by Peter Schmidleitner © Peter Schmidleitner Emergency Switch Compiled by Peter Schmidleitner © Peter Schmidleitner The mysterious Essential Bus Switch DA40-TDI G1000 Compiled by Peter Schmidleitner © Peter Schmidleitner Switch location Compiled by Peter Schmidleitner © Peter Schmidleitner When is it used ? n When the generator fails n to disconnect unnecessary electrical consumers n to supply battery power to essential electrical consumers 18/03/14 33 Compiled by Peter Schmidleitner © Peter Schmidleitner Essential Electrial Power n Essential Bus n PFD n Horizon *) n AHRS n ADC n Flaps n Landing light n Pitot Heating n Landing Light n Flood Light *) *) Emergency Battery n COM 1 n GPS / NAV Receiver 1 n Transponder n Engine instruments n Hot Battery Bus n (Essential Bus) n Pilot‘s map/reading light n Auxiliary jack Compiled by Peter Schmidleitner © Peter Schmidleitner n Main unserviceable systems n Fuel x-fer pump n MFD n Acionic / CDU fan n Position light, Strobe lights, Taxi light n Instrument lights, Map light n Starter n (Avionics Bus) n COM2, NAV/GPS2, ADF, DME, WX500, Audio, Autopilot Essential Electrial Power Compiled by Peter Schmidleitner © Peter Schmidleitner What happens ... n ... if it is switched ON during normal operation? n Will the battery be discharged? n NO ! Compiled by Peter Schmidleitner © Peter Schmidleitner Normal Situation Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery is charged DA40-TDI G1000, Ess. Bus switch 18/03/14 34 Compiled by Peter Schmidleitner © Peter Schmidleitner GEN u/s, Ess. PWR OFF Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery will be discharged DA40-TDI G1000, Ess. Bus switch Compiled by Peter Schmidleitner © Peter Schmidleitner GEN u/s, Ess. PWR ON Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery will be discharged at slow rate DA40-TDI G1000, Ess. Bus switch Compiled by Peter Schmidleitner © Peter Schmidleitner GEN OK, Ess. PWR ON Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus Battery is still charged DA40-TDI G1000, Ess. Bus switch Compiled by Peter Schmidleitner © Peter Schmidleitner Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus DA40-TDI G1000, Ess. Bus switch Essential Bus ON by mistake COM2, NAV/GPS2, Audio, ADF, DME, Autopilot WX 500 Fuel x-fer pump MFD Avion./CDU fan FAN / OAT indication Position light Strobe lights Taxi light, Map light Instrument lights Starter 18/03/14 35 Compiled by Peter Schmidleitner © Peter Schmidleitner n A very special engine start problem: n Start witch ON n Nothing happens! n Why? n Essential Bus switch ON by mistake! DA40-TDI G1000, Ess. Bus switch Compiled by Peter Schmidleitner © Peter Schmidleitner Hot Battery Bus Battery Bus Essential Bus GEN BATT Avioniic Bus ECU Bus Main Bus DA40-TDI G1000, Ess. Bus switch COM2, NAV/GPS2, Audio, ADF, DME, Autopilot WX 500 Fuel x-fer pump MFD Avion./CDU fan FAN / OAT indication Position light Strobe lights Taxi light, Map light Instrument lights Starter A very special engine start problem Essential Bus ON by mistake No power on Main Bus, therefore no starter ! Compiled by Peter Schmidleitner © Peter Schmidleitner DA40 TDI G1000 Electrical System Generator + Battery Fail ON ECU backup battery Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Autopilot 18/03/14 36 Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot limitations Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot Pitch Wrng Roll Wrng AP ON/OFF HDG select NAV mode APR mode Backbeam ALT Hold +/- V/S or +/- Alt Set Altitude or Baro Baro display/ setting ALT ARM Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot ALT V/S BARO display ALT Alert Pitch trim annunciator AP engaged annunciator Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot Pitch Mode: VS ALT ARM ALT GS Roll Mode: ROL HDG NAV ARM NAV APR ARM APR REV ARM REV GS ARM 18/03/14 37 Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot Vertical Speed Mode Toggles between ALT HLD and V/S Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot Altitude Hold Mode Toggles between ALT HLD and V/S Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot Altitude Preselect Select Altitude ALT ARM Change to V/S Select V/S ALT Hold and ALERT Compiled by Peter Schmidleitner © Peter Schmidleitner Autopilot AP disconnect CWS Manual Electric Trim 18/03/14 38 Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Performance Compiled by Peter Schmidleitner © Peter Schmidleitner The „DA 40 TDI“ and „Density Altitude“ n Attention! n Performance data which are engine- power dependant cannot be determined by just using „Density Altitude“! n Reason: the engine power output does not correspond to density altitude but pressure and temperature have their own, independent influence n This is a feature of the ECU controlled, turbocharged Diesel-engine Compiled by Peter Schmidleitner © Peter Schmidleitner Cruise Power Setting Compiled by Peter Schmidleitner © Peter Schmidleitner Cruising Speed e.g. 6000 ft, ISA, 70 % 121 kts 18/03/14 39 Compiled by Peter Schmidleitner © Peter Schmidleitner TOD SL, ISA, 1150 kg: 640 m Compiled by Peter Schmidleitner © Peter Schmidleitner TKOF Distance Compiled by Peter Schmidleitner © Peter Schmidleitner TKOF Run Compiled by Peter Schmidleitner © Peter Schmidleitner Grass Runway Length of grass TKOF roll Wet grass - 5 cm + 10% may be significantly longer 5 - 10 cm + 15% >10 cm min + 25% 18/03/14 40 Compiled by Peter Schmidleitner © Peter Schmidleitner Take off climb 66 KIAS Attention! Increasing downward Compiled by Peter Schmidleitner © Peter Schmidleitner Cruise Climb 73 KIAS Compiled by Peter Schmidleitner © Peter Schmidleitner ROC to gradient conversion Compiled by Peter Schmidleitner © Peter Schmidleitner LD, LR tabular format Flaps LDG VREF 71 KIAS Flaps UP VREF 73 KIAS 18/03/14 41 Compiled by Peter Schmidleitner © Peter Schmidleitner Landing Distance Compiled by Peter Schmidleitner © Peter Schmidleitner Landing Run Compiled by Peter Schmidleitner © Peter Schmidleitner Grass Runway Length of grass LDG run Wet grass - 5 cm + 5% may be significantly longer 5 - 10 cm + 15% >10 cm min + 25% Compiled by Peter Schmidleitner © Peter Schmidleitner Go Around 18/03/14 42 Compiled by Peter Schmidleitner © Peter Schmidleitner Obstacles ? RWL TOD Obst. Dist. „d“ „h“ „d“= (RWL + Obst.Dist.) - TOD Gradient = („h“ / „d“) * 100 Compiled by Peter Schmidleitner © Peter Schmidleitner Vöslau RWY 31 950 650 830 m 1130 98 ft „d“= (950 + 830) – 650 = 1130 Gradient = (30 / 1130) * 100 = 2,65 % Acc. Performance Graph: ~ 9 % Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Mass and Balance Compiled by Peter Schmidleitner © Peter Schmidleitner Empty Mass n Empty Mass includes: n Equipment as per Equipment Inventory n Brake fluid n Coolant fluid n Gear oil n Engine oil n Unusable fuel (2 x 1,0 USG) 18/03/14 43 Compiled by Peter Schmidleitner © Peter Schmidleitner Center of Gravity Envelope 2.46 2.59 Compiled by Peter Schmidleitner © Peter Schmidleitner Moment Envelope Compiled by Peter Schmidleitner © Peter Schmidleitner Moment Arms Item Lever Arm (m) Front seats 2.30 Rear seats 3.25 Wing tanks 2.63 Fwd. baggage 3.89 Aft baggage 4.54 Compiled by Peter Schmidleitner © Peter Schmidleitner Typical M+B data Empty mass Moment CG arm „IFR“-version (ADF, WX500) 833,5 2057,7 2,469 „N-VFR“-version 826,2 2032,3 2,460 18/03/14 44 Compiled by Peter Schmidleitner © Peter Schmidleitner M&B Calculation Lever arm Mass (kg) Moment (kgm) Empty mass 2.47 830 2050.1 Front seats 2.30 Rear seats 3.25 Fwd. Baggage 3.89 Zero Fuel Mass Fuel 2.63 Total TKOF Mass 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 170 x 2.30 = 391.0 80 x 3.25 = 260.0 ~20 USG Compiled by Peter Schmidleitner © Peter Schmidleitner M&B Calculation Lever arm Mass (kg) Moment (kgm) Empty mass 2.47 830 2050.1 Front seats 2.30 Rear seats 3.25 Fwd. Baggage 3.89 Zero Fuel Mass Fuel 2.63 Total TKOF Mass 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 2740.0 : 1090 = 2.514 2897.8 : 1150 = 2.52 2.514 2.52 Compiled by Peter Schmidleitner © Peter Schmidleitner ZFM 1090 kg , 2.514 m TOM 1150 kg , 2.52 m Center of Gravity Envelope Compiled by Peter Schmidleitner © Peter Schmidleitner M&B Calculation Lever arm Mass (kg) Moment (kgm) Empty mass 2.47 830 2050.1 Front seats 2.30 Rear seats 3.25 Fwd. Baggage 3.89 Zero Fuel Mass Fuel 2.63 Total TKOF Mass 80 170 10 1090 60 1150 391.0 260.0 38.9 2740.0 157.8 2897.8 18/03/14 45 Compiled by Peter Schmidleitner © Peter Schmidleitner Moment Envelope ZFM 1090 kg , 2740.0 TOM 1150 kg , 2897.8 Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Emergency Equipment Compiled by Peter Schmidleitner © Peter Schmidleitner Emergency equipment Compiled by Peter Schmidleitner © Peter Schmidleitner Emergency Exit FWD 1 2 18/03/14 46 Compiled by Peter Schmidleitner © Peter Schmidleitner Emergency Exit FWD 1 2 Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Kinds of Operation Equipment List (KOEL) Compiled by Peter Schmidleitner © Peter Schmidleitner Kinds of Operation Equipment List KOEL Compiled by Peter Schmidleitner © Peter Schmidleitner Kinds of Operation Equipment List KOEL 18/03/14 47 Compiled by Peter Schmidleitner © Peter Schmidleitner Kinds of Operation Equipment List KOEL Compiled by Peter Schmidleitner © Peter Schmidleitner Kinds of Operation Equipment List KOEL Compiled by Peter Schmidleitner © Peter Schmidleitner Additional minimum equipment for the intended operation may be required by national operating rules and also depends on the route to be flown. Kinds of Operation Equipment List KOEL Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Servicing 18/03/14 48 Compiled by Peter Schmidleitner © Peter Schmidleitner Scheduled maintenance n Every n 100 hours n 200 hours n 1000 hours n 2000 hours n Annually Compiled by Peter Schmidleitner © Peter Schmidleitner Refuelling Compiled by Peter Schmidleitner © Peter Schmidleitner De-icing n Approved de-icing fluids: n Kilfrost TKS 80 n Aeroshell Compound 07 n Procedure: n Remove snow with brush n Spray de-icing fluid n Wipe dry Compiled by Peter Schmidleitner © Peter Schmidleitner Control surfaces gust lock 18/03/14 49 Compiled by Peter Schmidleitner © Peter Schmidleitner Mooring Compiled by Peter Schmidleitner © Peter Schmidleitner Mooring Compiled by Peter Schmidleitner © Peter Schmidleitner Tow bar Diamond DA40-TDI G1000 Compiled by Peter Schmidleitner Flight Procedures 18/03/14 50 Compiled by Peter Schmidleitner © Peter Schmidleitner TKOF Profile Rotate at 59 kt Compiled by Peter Schmidleitner © Peter Schmidleitner LDG Profile Compiled by Peter Schmidleitner © Peter Schmidleitner Checklists The checklists are not part of the AFM, and they are not „officially Diamond-endorsed“. They are a recommendation for „Operator Checklists“ published by „Diamond Aircraft Flight Training Division“. Compiled by Peter Schmidleitner © Peter Schmidleitner Thank you for your attention!